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Selection of Some Rotor Parameters to Reduce Pitch Roll Coupling of Helicopter Flight Dynamics

Selection of Some Rotor Parameters to Reduce Pitch Roll Coupling of Helicopter Flight Dynamics

  • 18 pages
  • SKU # : sm_1980_RS-Design_0821_Chen

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Selection of Some Rotor Parameters to Reduce Pitch Roll Coupling of Helicopter Flight Dynamics

Authors / Details: Robert T. N. Chen, NASA Ames Research Center